一种基于伪速率调制器的自激振荡消除姿态控制方法

doi:10.3969/j.issn.1674 1579.2022.06.005

Abstract

Abstract: A closed loop control system based on pseudo rate modulator (PRM) may frequently oscillate due to its strongly nonlinear feature and uncertainty. And propellants exhausts extra when control system oscillates. A method is given to eliminate self excited oscillation via identifying the self excited oscillation period. The control parameters are modified according to the identification results. Finally the simulation results show that the given method is valid.

Key words: self excited oscillation, attitude control, Psudo rate modulator

CLC Number:

V448

LIN Bo, CHANG JianSong, LIU Xinyan. An Attitude Control Method Based on Pseudo Rate Modulator for Eliminating Self Excited Oscillation[J].Aerospace Contrd and Application, 2022, 48(6): 40-45.

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URL: http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/10.3969/j.issn.1674 1579.2022.06.005

http://journal01.magtech.org.cn/Jwk3_kjkzjs/EN/Y2022/V48/I6/40

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An Attitude Control Method Based on Pseudo Rate Modulator for Eliminating Self Excited Oscillation

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